ES2300247T3 - Inyector de combustible liquido para quemadores de turbinas de gas. - Google Patents

Inyector de combustible liquido para quemadores de turbinas de gas. Download PDF

Info

Publication number: ES2300247T3
Authority: ES; Spain
Prior art keywords: compressed air; liquid fuel; gas turbine; injector; holes
Prior art date: 1999-05-31
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.): Expired - Lifetime

Application number

ES00304601T

Other languages

English (en)

Spanish (es)

Inventor

Anthony Dean

Alessio Miliani

Luciano Mei

Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)

Nuovo Pignone Holding SpA

Nuovo Pignone SpA

Original Assignee

Nuovo Pignone Holding SpA

Nuovo Pignone SpA

Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)

1999-05-31

Filing date

2000-05-31

Publication date

2008-06-16

2000-05-31 Application filed by Nuovo Pignone Holding SpA, Nuovo Pignone SpA filed Critical Nuovo Pignone Holding SpA

2008-06-16 Application granted granted Critical

2008-06-16 Publication of ES2300247T3 publication Critical patent/ES2300247T3/es

2020-05-31 Anticipated expiration legal-status Critical

Status Expired - Lifetime legal-status Critical Current

Links

239000000446 fuel Substances 0.000 title claims abstract description 61
239000007788 liquid Substances 0.000 title claims abstract description 51
RLQJEEJISHYWON-UHFFFAOYSA-N flonicamid Chemical compound FC(F)(F)C1=CC=NC=C1C(=O)NCC#N RLQJEEJISHYWON-UHFFFAOYSA-N 0.000 title 1
238000011144 upstream manufacturing Methods 0.000 claims abstract description 4
238000002485 combustion reaction Methods 0.000 description 7
239000000203 mixture Substances 0.000 description 3
230000000694 effects Effects 0.000 description 2
239000012530 fluid Substances 0.000 description 2
238000000889 atomisation Methods 0.000 description 1
239000011248 coating agent Substances 0.000 description 1
238000000576 coating method Methods 0.000 description 1
239000012212 insulator Substances 0.000 description 1
238000002955 isolation Methods 0.000 description 1
238000000034 method Methods 0.000 description 1
238000002156 mixing Methods 0.000 description 1
238000000926 separation method Methods 0.000 description 1

Classifications

- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
- F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
- F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
- F23R3/04—Air inlet arrangements
- F23R3/10—Air inlet arrangements for primary air
- F23R3/12—Air inlet arrangements for primary air inducing a vortex
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23D—BURNERS
- F23D11/00—Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space
- F23D11/10—Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space the spraying being induced by a gaseous medium, e.g. water vapour
- F23D11/101—Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space the spraying being induced by a gaseous medium, e.g. water vapour medium and fuel meeting before the burner outlet
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
- F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
- F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
- F23R3/286—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply having fuel-air premixing devices

Landscapes

Engineering & Computer Science (AREA)
Chemical & Material Sciences (AREA)
Combustion & Propulsion (AREA)
Mechanical Engineering (AREA)
General Engineering & Computer Science (AREA)
Fuel-Injection Apparatus (AREA)
Nozzles (AREA)
Gas Burners (AREA)

ES00304601T 1999-05-31 2000-05-31 Inyector de combustible liquido para quemadores de turbinas de gas. Expired - Lifetime ES2300247T3 (es)

Applications Claiming Priority (2)

Application Number	Priority Date	Filing Date	Title
ITMI99A1204		1999-05-31
IT1999MI001204A ITMI991204A1 (it)	1999-05-31	1999-05-31	Iniettore di combustibile liquido per bruciatori in turbine a gas

Publications (1)

Publication Number	Publication Date
ES2300247T3 true ES2300247T3 (es)	2008-06-16

Family

ID=11383079

Family Applications (1)

Application Number	Title	Priority Date	Filing Date
ES00304601T Expired - Lifetime ES2300247T3 (es)	1999-05-31	2000-05-31	Inyector de combustible liquido para quemadores de turbinas de gas.

Country Status (12)

Country	Link
US (1)	US6334309B1 (fr)
EP (1)	EP1058063B1 (fr)
AR (1)	AR024165A1 (fr)
BR (1)	BR0002534A (fr)
DE (1)	DE60037850T2 (fr)
DZ (1)	DZ3084A1 (fr)
EG (1)	EG22570A (fr)
ES (1)	ES2300247T3 (fr)
IT (1)	ITMI991204A1 (fr)
MX (1)	MXPA00005371A (fr)
NO (1)	NO330494B1 (fr)
RU (1)	RU2224953C2 (fr)

Families Citing this family (29)

* Cited by examiner, † Cited by third party
Publication number	Priority date	Publication date	Assignee	Title
DE10160997A1 (de)	2001-12-12	2003-07-03	Rolls Royce Deutschland	Magervormischbrenner für eine Gasturbine sowie Verfahren zum Betrieb eines Magervormischbrenners
JP4414769B2 (ja) *	2002-04-26	2010-02-10	ロールス−ロイス・コーポレーション	ガスタービンエンジン燃焼器用の燃料予混合モジュール
DE10219354A1 (de) *	2002-04-30	2003-11-13	Rolls Royce Deutschland	Gasturbinenbrennkammer mit gezielter Kraftstoffeinbringung zur Verbesserung der Homogenität des Kraftstoff-Luft-Gemisches
US7007486B2 (en) *	2003-03-26	2006-03-07	The Boeing Company	Apparatus and method for selecting a flow mixture
US7127899B2 (en) *	2004-02-26	2006-10-31	United Technologies Corporation	Non-swirl dry low NOx (DLN) combustor
WO2007051705A1 (fr) *	2005-11-04	2007-05-10	Alstom Technology Ltd	Lance à combustible
EP2023041A1 (fr) *	2007-07-27	2009-02-11	Siemens Aktiengesellschaft	Brûleur à prémélange et procédé de mise en oeuvre du brûleur
DE102007043626A1 (de)	2007-09-13	2009-03-19	Rolls-Royce Deutschland Ltd & Co Kg	Gasturbinenmagerbrenner mit Kraftstoffdüse mit kontrollierter Kraftstoffinhomogenität
US20100089022A1 (en) *	2008-10-14	2010-04-15	General Electric Company	Method and apparatus of fuel nozzle diluent introduction
US9121609B2 (en)	2008-10-14	2015-09-01	General Electric Company	Method and apparatus for introducing diluent flow into a combustor
US20100089020A1 (en) *	2008-10-14	2010-04-15	General Electric Company	Metering of diluent flow in combustor
US8567199B2 (en) *	2008-10-14	2013-10-29	General Electric Company	Method and apparatus of introducing diluent flow into a combustor
EP2253888B1 (fr) *	2009-05-14	2013-10-16	Alstom Technology Ltd	Brûleur d'une turbine à gaz ayant un générateur de vortex avec une lance à combustible
US9010119B2 (en) *	2010-11-03	2015-04-21	General Electric Company	Premixing nozzle
US20130232978A1 (en) *	2012-03-12	2013-09-12	Zhongtao Dai	Fuel air premixer for gas turbine engine
EP2743588A1 (fr)	2012-12-11	2014-06-18	Siemens Aktiengesellschaft	Positionnement d'injecteur de carburant en retrait
US9759425B2 (en) *	2013-03-12	2017-09-12	General Electric Company	System and method having multi-tube fuel nozzle with multiple fuel injectors
US9671112B2 (en)	2013-03-12	2017-06-06	General Electric Company	Air diffuser for a head end of a combustor
US9534787B2 (en)	2013-03-12	2017-01-03	General Electric Company	Micromixing cap assembly
US9765973B2 (en)	2013-03-12	2017-09-19	General Electric Company	System and method for tube level air flow conditioning
US9651259B2 (en)	2013-03-12	2017-05-16	General Electric Company	Multi-injector micromixing system
US9528444B2 (en)	2013-03-12	2016-12-27	General Electric Company	System having multi-tube fuel nozzle with floating arrangement of mixing tubes
US9650959B2 (en)	2013-03-12	2017-05-16	General Electric Company	Fuel-air mixing system with mixing chambers of various lengths for gas turbine system
JP6191918B2 (ja) *	2014-03-20	2017-09-06	三菱日立パワーシステムズ株式会社	ノズル、バーナ、燃焼器、ガスタービン、ガスタービンシステム
US10288291B2 (en) *	2014-08-15	2019-05-14	General Electric Company	Air-shielded fuel injection assembly to facilitate reduced NOx emissions in a combustor system
KR101657535B1 (ko) *	2015-05-21	2016-09-19	두산중공업 주식회사	버닝 저감 연료공급노즐.
DE102017223113A1 (de) *	2017-12-18	2019-06-19	Sms Group Gmbh	Brenner
KR102119879B1 (ko) *	2018-03-07	2020-06-08	두산중공업 주식회사	파일럿 연료 분사 장치, 이를 구비한 연료 노즐 및 가스 터빈
US11371708B2 (en) *	2018-04-06	2022-06-28	General Electric Company	Premixer for low emissions gas turbine combustor

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number	Priority date	Publication date	Assignee	Title
US4198815A (en)	1975-12-24	1980-04-22	General Electric Company	Central injection fuel carburetor
SU1553793A1 (ru) *	1987-05-04	1990-03-30	Научно-производственное объединение по топливной аппаратуре двигателей "ЦНИТА"	Жарова труба камеры сгорани
US4880194A (en) *	1987-07-21	1989-11-14	John Geise	Apparatus and method for supporting articles
US4854127A (en) *	1988-01-14	1989-08-08	General Electric Company	Bimodal swirler injector for a gas turbine combustor
US5394688A (en) *	1993-10-27	1995-03-07	Westinghouse Electric Corporation	Gas turbine combustor swirl vane arrangement
US5461865A (en)	1994-02-24	1995-10-31	United Technologies Corporation	Tangential entry fuel nozzle
US5822992A (en)	1995-10-19	1998-10-20	General Electric Company	Low emissions combustor premixer
US5778676A (en)	1996-01-02	1998-07-14	General Electric Company	Dual fuel mixer for gas turbine combustor
DE19803879C1 (de) *	1998-01-31	1999-08-26	Mtu Muenchen Gmbh	Zweistoffbrenner

1999
- 1999-05-31 IT IT1999MI001204A patent/ITMI991204A1/it unknown
2000
- 2000-05-26 US US09/579,510 patent/US6334309B1/en not_active Expired - Lifetime
- 2000-05-29 DZ DZ000096A patent/DZ3084A1/fr active
- 2000-05-30 RU RU2000113796/06A patent/RU2224953C2/ru active
- 2000-05-30 NO NO20002764A patent/NO330494B1/no not_active IP Right Cessation
- 2000-05-31 EG EG20000712A patent/EG22570A/xx active
- 2000-05-31 MX MXPA00005371A patent/MXPA00005371A/es unknown
- 2000-05-31 DE DE60037850T patent/DE60037850T2/de not_active Expired - Lifetime
- 2000-05-31 EP EP00304601A patent/EP1058063B1/fr not_active Expired - Lifetime
- 2000-05-31 ES ES00304601T patent/ES2300247T3/es not_active Expired - Lifetime
- 2000-05-31 BR BR0002534-8A patent/BR0002534A/pt not_active IP Right Cessation
- 2000-05-31 AR ARP000102684A patent/AR024165A1/es not_active Application Discontinuation

Also Published As

Publication number	Publication date
NO20002764L (no)	2000-12-01
DE60037850D1 (de)	2008-03-13
DZ3084A1 (fr)	2004-06-20
EP1058063B1 (fr)	2008-01-23
ITMI991204A0 (it)	1999-05-31
EG22570A (en)	2003-04-30
NO20002764D0 (no)	2000-05-30
DE60037850T2 (de)	2009-01-22
NO330494B1 (no)	2011-05-02
RU2224953C2 (ru)	2004-02-27
BR0002534A (pt)	2001-05-22
ITMI991204A1 (it)	2000-12-01
US6334309B1 (en)	2002-01-01
EP1058063A1 (fr)	2000-12-06
MXPA00005371A (es)	2002-04-24
AR024165A1 (es)	2002-09-04

Publication	Publication Date	Title
ES2300247T3 (es)	2008-06-16	Inyector de combustible liquido para quemadores de turbinas de gas.
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ES2286231T3 (es)	2007-12-01	Encendedor tubular de gas.
JP5476462B2 (ja)	2014-04-23	マルチプレミキサ燃料ノズル
RU2000113796A (ru)	2002-06-20	Инжектор для жидкого топлива, предназначенный для горелок в газовых турбинах
US11859822B2 (en)	2024-01-02	Burner assembly, gas turbine combustor, and gas turbine
CN102087026A (zh)	2011-06-08	二次燃料喷嘴中的燃料喷射
US20230022725A1 (en)	2023-01-26	Burner assembly, gas turbine combustor, and gas turbine
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US12247522B2 (en)	2025-03-11	Burner assembly, gas turbine combustor, and gas turbine
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